Methods and systems for designing a composite structure

Patent metadata

Field	Value
Publication number	US-10983078-B2
Application number	US-201916691896-A
Country	US
Kind code	B2
Filing date	Nov 22, 2019
Priority date	Jun 22, 2015
Publication date	Apr 20, 2021
Grant date	Apr 20, 2021

Abstract

A computer-implemented method of determining moisture content of a composite structure is provided. The method includes performing a thermal analysis calculation on the composite structure to determine a temporal surface temperature profile of the composite structure based on temporal environmental parameter profiles, wherein the surface temperature profile is determined independently of a moisture content of the composite structure. The method also includes performing a moisture content analysis calculation on the composite structure to determine a moisture content of the composite structure, wherein the moisture content analysis calculation is based on the determined temporal surface temperature profile and a thickness of the composite structure. The thermal analysis calculation is performed iteratively with a first time period and the moisture content analysis calculation is performed iteratively with a second time period that is longer than the first time period.

First claim

What is claimed is:

1. A method of designing and manufacturing composite structures for use in aircraft, said method comprising:
performing a thermal analysis on a model composite structure to determine a temporal surface temperature profile of the model composite structure based on temporal environmental parameter profiles associated with at least one location in which the model composite structure is selectively positionable, the temporal environmental parameter profiles determined based on environmental data collected by at least one sensor at the at least one location,
performing a moisture content analysis on the model composite structure, wherein the moisture content analysis is based on the determined temporal surface temperature profile and a desired thickness of a composite structure to be manufactured, wherein the temporal surface temperature profile is determined independently of the moisture content analysis,
wherein the thermal analysis is performed iteratively with a first time period and the moisture content analysis is performed iteratively with a second time period that is longer than the first time period;
determining an allowable moisture content of the model composite structure based on the moisture content analysis;
determining a number of plies of material within the desired thickness of the composite structure sufficient to maintain the allowable moisture content;
designing the composite structure based on the determined number of plies of material; and
manufacturing the composite structure based on the design that includes the number of plies of material.

2. The method according to claim 1 , wherein performing a thermal analysis based on temporal environmental parameter profiles comprises receiving environmental parameter data related to a plurality of environmental parameters from an environmental parameter database, the plurality of environmental parameters including temperature, solar load, wind speed, and rainfall, wherein the environmental parameter data is collected from a plurality of airports, in which the model composite structure is selectively positionable, over a predetermined time period.

3. The method according to claim 2 , further comprising determining a temporal environmental parameter profile for each environmental parameter of the plurality of environmental parameters.

4. The method according to claim 1 , wherein performing the thermal analysis comprises:
monitoring at least one weather parameter that includes temperature, solar load, wind speed, and rainfall at a location in which the model composite structure is selectively positionable; and
determining the temporal surface temperature profile based on the monitored weather parameter.

5. The method according to claim 1 , wherein performing the moisture content analysis comprises:
determining a relative humidity at each of a plurality of airports in which the model composite structure is selectively positionable as a component of an aircraft traveling between the plurality of airports; and
wherein performing the moisture content analysis on the model composite structure is based on the determined relative humidity at which the model composite structure is selectively positionable.

6. The method according to claim 1 further comprising:
determining a fleet utilization profile for each airport of a plurality of airports, wherein each fleet utilization profile is based on in-flight operating data and grounded non-operating data for aircraft, formed from at least one composite structure, operating from each airport of the plurality of airports, wherein a temperature difference is defined based on whether the aircraft is in-flight, defined by a first temperature, versus being grounded, defined by a second temperature; and
performing the thermal analysis on the model composite structure associated with the aircraft based on the temperature difference.

7. A system for use in designing composite structures for use in aircraft, the system comprising:
an environmental parameter database comprising environmental parameter data, related to a plurality of environmental parameters, collected by at least one sensor at a plurality of airports;
a computing device comprising a processor configured to:
generate a plurality of temporal environmental parameter profiles based on the environmental parameter data, wherein each environmental parameter profile is based on an environmental parameter of the plurality of environmental parameters,
perform a thermal analysis to generate a temporal surface temperature profile of a model composite structure for the plurality of airports, wherein the temporal surface temperature profile is generated based on the generated temporal environmental parameter profiles;
perform a moisture content analysis based on the generated temporal surface temperature profile and a desired thickness of a composite structure to be manufactured, wherein the surface temperature profile is generated independently of the moisture content analysis;
determine an allowable moisture content of the model composite structure based on the moisture content analysis;
determine a number of plies of material within the desired thickness of the composite structure sufficient to maintain the allowable moisture content; and
design the composite structure based on the determined number of plies of material for obtaining the desired thickness of the composite structure having a moisture content percentage by weight of the composite structure that is less than a fully saturated level, the number of plies determined based on the environmental parameter profiles and on predetermined composite structure data,

wherein the thermal analysis is performed iteratively with a first time period and the moisture content analysis is performed iteratively with a second time period that is longer than the first time period.

8. The system according to claim 7 , wherein the processor is further configured to generate the temporal environmental parameter profiles based on at least one of: temperature, solar load, wind speed, and rainfall at a location in which the composite structure is selectively positionable.

9. The system according to claim 7 , wherein the processor is further configured to generate the temporal environmental parameter profiles further based on an ambient relative humidity at the plurality of airports in which the composite structure is selectively positionable.

10. The system according to claim 7 , wherein the processor is further configured to generate the temporal environmental parameter profiles based on in-flight operating data and grounded non-operating data for aircraft, formed from at least one composite structure, operating from each airport of the plurality of airports, wherein a temperature difference is defined based on whether the aircraft associated with the model composite structure is in-flight, defined by a first temperature, versus being grounded, defined by a second temperature.

11. The system according to claim 10 , further comprising a composite structure database configured to store data related to the model composite structure, wherein the processor is further configured to determine the moisture content of the model composite structure based on the composite structure data.

12. At least one non-transitory computer-readable storage media having computer-executable instructions embodied thereon, wherein when executed by at least one processor, the computer-executable instructions cause the at least one processor to:
generate a plurality of temporal environmental parameter profiles based on environmental parameter data collected by at least one sensor at a plurality

Assignees

• Boeing Co

Inventors

• Apdalhaliem Sahrudine
• Chen Heh-Chyun Cliff
• Ashmawi Waeil M
• Meredith Kimberly D

Classifications

• G01N17/00 Primary

  Investigating resistance of materials to the weather, to corrosion, or to light · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• G06F30/20 Primary

  Design optimisation, verification or simulation (optimisation, verification or simulation of circuit designs G06F30/30) · CPC title

• G01N25/00 Primary

  Investigating or analyzing materials by the use of thermal means (G01N3/00 - G01N23/00 take precedence) · CPC title

• G01N5/025 Primary

  for determining moisture content · CPC title